Mitered mechanical switches

ABSTRACT

An improved phased-array active antenna transmit-receive means utilizing a multiplicity of individual transmit-receive cells positioned in an array format upon a common wafer of semiconductor material. Each transmit-receiver cell, comprises a multiplicity of redundant, integrated circuit, electronic devices implanted upon the common semiconductor substrate. The transmit-receive cells utilize novel mitered mechanical switches to permanently interconnect individual electronic devices into either transmit or receive circuits during the fabrication and test of the transmit-receive cells. Radio frequency and direct current input and output vias formed from a novel metal evaporation technique connect the devices upon the surface of the common semiconductor wafer to underlying, insulated direct current distribution circuits and a radio frequency manifold. This array of improved phased-array active antenna transmit-receive means comprised of transmit-receive cells sharing common central processing means, logic control and heat dissipation means results in a significant reduction in the size and weight of the standard phased-array active antenna system. This significant reduction in antenna system size and weight is very important in broad band electronic countermeasure systems or narrow band phased array active antenna radar systems as used in advanced tactical fighters, or space applications.

This is a division of application Ser. No. 07/013,490 filed Feb. 11,1987, now U.S. Pat. No. 4,823,136 issued Apr. 18, 1989.

BACKGROUND OF THE INVENTION

1. Field of the Invention

The present invention relates to an a small, light weighttransmit-receive means for use in a phased-array active antenna systemutilizing a multiplicity of individual transmit-receive cells, allmounted upon a common wafer of semiconductor material. Eachtransmit-receive cell comprises a plurality of redundant electronicdevices that are selectively and permanently interconnectable by miteredmechanical switches.

2. Description of the Prior Art

Previous phased array active antenna systems for radar or electronicwarfare applications utilized active FETs (field effect transistors),passive capacitors and phase shifting microstrip lines all manufacturedon a multiplicity of individual monolithic chips. Each individual chipperformed a separate functions such as; attenuation, digital and analogphase shift, power amplification, transmit/receive duplexing, andlow-noise amplification. All of the individual chips were then mountedtogether on a cooled platen in a metallic assembly. This aggregation ofindividual chips constituted only one active element of a phased-arrayactive antenna system. A complete phased-array active antenna systemrequired hundreds of such complex elements all mounted to a commonmatrix of radio frequency signal carriers.

Today, there are radar and electronic warfare applications, wherelightweight active antenna systems are necessary. A prior art assemblyof monolithic chips bonded onto a heavy metal matrix of carriers weighedover 600 lbs. (272.73 kgm). When a high speed, advanced tacticalaircraft, performs high velocity tactical maneuvers; such a heavy,phased array active antenna radar or electronic warfare system would besubjected to high inertial forces. Only a lightweight, phased arrayactive antenna system would be able to successfully withstand the highvelocity turns and extreme gravitational forces developed by an advancedtactical fighter.

A standard phased-array active antenna system comprises; a means toproduce a radio frequency signal, a transmit-receive means or duplexerwhich is operable to transmit or receive radio frequency signals, and alogic device, operable to shape the output beam from an antenna means.

The transmit-receive means or duplexer comprises; an attenuation means,a multistage amplification means, a low-noise amplification means, andappropriate transmit-receive switches which operate as a signalisolation means when the transmit-receive means is in either a transmitor receipt mode. Heat dissipation of heat away from the amplificationmeans of the duplexer requires the use of heat sinks integrated with theduplexer to maintain operational temperatures for the circuits. Directcurrent, electrical energy is provided from a power generation means tothe transmit-receive means devices.

Historically, a variety of systems of decreasing weight and size havebeen designed to achieve a lightweight antenna phased-array system. Thepatent to Stockton et al., U.S. Pat. No. 4,490,721 taught a monolithicmicrowave circuit including an integral array antenna. The Stocktoninvention included radiating elements, a feed network, phasing network,active and passive semiconductor devices, logic interface, and amicroprocessor all incorporated on a gallium arsenide substrate.However, even with the incorporation of these devices on one substratethe Stockton invention perpetuated the individual element approach.Also, the lack of electronic device redundancy resulted in a low yieldof operable chips. The reliance on this individual chip approach did notappreciably reduce the weight of the final antenna array with itsmultiplicity of individual elements. A multiple device or electronicdevice redundancy concept in the transmit-receive means would produce ahigh yield transmit-receive means. If a multiplicity of transmit-receivemeans are mounted onto a common semiconductor wafer a greater yield ofoperable devices would be the result.

The size of the antenna unit cell is constrained in that it cannot beany larger than 0.6 λ_(O) is the free space wavelength given by thisequation: ##EQU1##

The problem to be solved, then, is the manufacture of an activephased-array antenna system incorporating lightweight, redundant arrayelements operable for use in broadband radar or electronic warfaredevices on advanced tactical fighters.

SUMMARY OF THE INVENTION

In accordance with the above requirements, the present invention, aphased-array active antenna transmit-receive means utilizing arrayedtransmit-receive cells all mounted upon a common semiconductor substrateresolves the problem of multiple microelectronic modules and theirresultant combined weight. For frequencies equal to 12 GHz, 15 GHz or 18GHz triple electronic device redundancy can be incorporated into a spaceof 0.6 λ_(O) or approximately 0.5 in. (1.27 cm).

This transmit-receive means, operable for use in an active antennaphased array system would transmit or receive individually phase shiftedradio frequency signals. This transmit-receive means would comprise asingle wafer of semiconductor material. This wafer would be planar inconfiguration having a top and a bottom surface. A plurality ofindividual transmit-receive cells would be layered upon the top surfaceof this common wafer utilizing standard photolithographic techniques.These individual transmit-receive cells would comprise a multiplicity ofredundant electronic devices. These redundant electronic devices wouldbe selectively, permanently interconnectable to form transmit andreceive circuits on the surface of the wafer.

A critical component of these redundant devices would be a mechanicalswitching means that would be operable to selectively, permanentlyinterconnect the various selected electronic devices. This applicationteaches a mitered mechanical switch which is operable to selectivelyinterconnect various; attenuation, amplification or phase shiftingdevices during the transmit-receive means fabrication and test. Thesemechanical mitered switches are operable to be closed at roomtemperatures using standard pressure sensitive techniques.

To input and output radio frequency signals onto the transmit-receivemeans requires a via fabrication technique using metal evaporation toproduce stable, solid electrical connections. Further these same viascould be produced to supply direct current to the field effecttransistors of the various signal amplification devices on thetransmit-receive cell.

The disclosed transmit-receive means therefore comprises an array ofindividual transmit-receive cells. Each individual transmit-receive cellcomprises all of the necessary electronic devices to transmit or receivea radio frequency signal in a physical area of approximately 0.395inches (1.002 cm). Further, these devices are positioned upon theindividual transmit-receive cell in a state of triple redundancy.Mitered mechanical switches, which are closed using pressure orvibration applied at room temperature permits the selection andpermanent interconnection of individual operable electronic devices intotransmit or receive circuits. Further the individual devices haveredundant elements such as field effect transistors which increase theprobability of working devices, and operational transmit-receivecircuits, thereby increasing transmit-receive cell yield. All of theindividual transmit-receive cells are layered upon a single wafer ofsemiconductor material such as galium arsenide, in an arrayconfiguration. Each transmit-receive cell would control the individualoutput signal emitted from an individual antenna means or amplify thereceived signal from that same antenna means or amplify the receivedsignal from that same antenna means. An array of sixteentransmit-receive cells would be approximately 2.08 inches (5.28 cm) indiameter. An antenna system comprising one hundred of suchtransmit-receive means of sixteen cells each would be approximately 208inches (528.32 cm) in diameter with an overall weight of approximately60-80 lbs. (27.27-36.36 kg). Therefore, the use of this noveltransmit-receive means would have a ten-fold reduction in weight for theconventional active antenna radar system.

The transmit-receive cells are fully functional at broadband and narrowband radio frequencies. In the narrow band of 9.8 to 10.2 GHz, theactive antenna system would operate as a radar system. In the broadbandrange of 2.0 GHz to 20.0 GHz the active antenna system is fullyfunctional in electronic countermeasures and radio frequency jamming.Either application would find a place on an advanced tactical aircraftor space based configuration because of weight and size restrictions.

BRIEF DESCRIPTION OF THE DRAWINGS

For a better understanding of the invention, reference may be had to thepreferred embodiment exemplary of the invention shown in theaccompanying drawings in which:

FIG. 1 is a flowchart of the individual means necessary for a phasedarray active antenna system;

FIG. 2 is a flowchart of the individual means necessary for atransmit-receive means as used in a phased array active antenna system;

FIG. 3 is a plan view of sixteen transmit-receive cells on a singleuncut wafer of semiconductor material, three inch (7.62 cm) format;

FIG. 3A is a plan view of sixteen transmit-receive cells in a single,uncut wafer of semiconductor material, four inch (10.16 cm) format;

FIG. 3B is an exploded view of the array of sixteen transmit-receivecells on a single uncut wafer of semiconductor material, four inch(10.16 cm) format with sealed lid;

FIG. 4 is a chart showing the relative positions of the individual,redundant electronic devices on a single transmit-receive cell;

FIG. 5 is a schematic representation of the individual, redundantelectronic devices on a single transmit-receive cell;

FIG. 6 is a chart showing the relative positions of various groups ofdevices as they appear on the surface of an individual transmit-receivemeans;

FIG. 6A is a plan view of the devices located in the portion shown as Aon FIG. 6;

FIG. 6B is a plan view of the devices located in the portion shown as Bon FIG. 6;

FIG. 6C is a plan view of the devices located in the portion shown as Con FIG. 6;

FIG. 6D is a plan view of the devices located in the portion shown as Din FIG. 6;

FIG. 6E is a plan view of the devices located in the portion shown as Ein FIG. 6;

FIG. 7 is a plan view of the attenuator;

FIG. 7A is a plan view of the digital phase shifter;

FIG. 7B is a plan view enlargement of the left side of the digital phaseshifter;

FIG. 7C is a plan view enlargement of the right side of the digitalphase shifter;

FIG. 7D is a plan view of the analog phase shifters;

FIG. 7E is a plan view of the transmit-receive switch;

FIG. 7F is a plan view of the first stage amplifier;

FIG. 7G is a plan view of the driver stage amplifier;

FIG. 7H is a plan view of the output stage amplifier;

FIG. 7I is a plan view of the low noise amplifier;

FIG. 8 is a cross sectional of the manner of making the direct currentand radio frequency input/output vias within the common semiconductorwafer;

FIG. 8A is a cross sectional of the manner of making the input/outputvias with thin-sputtered metalization layer and photo-resist layer;

FIG. 8B is a cross section manner of making the plated Au layer upon thethin-sputtered metalization layer;

FIG. 8C is a cross section manner of utilizing the shadow mask layer;

FIG. 8D is a cross section manner of making the evaporated metalinterconnect layer;

FIG. 8E is a cross section manner of making the completed input/outputvia in conjunction with the radio frequency and direct current manifoldlayers;

FIG. 9 is a plan view of a mitered mechanical switch in the openposition;

FIG. 9A is a plan view of the first layer of metalization of the miteredmechanical switch in FIG. 10;

FIG. 9B is a plan view of the second layer of metalization of themitered mechanical switch in FIG. 10;

FIG. 9C is a plan view of the third layer of metalization of the miteredmechanical switch in FIG. 10;

FIG. 9D is a side elevational view, left of the mitered mechanicalswitch of FIG. 10;

FIG. 9E is a side elevational view, right of the mitered mechanicalswitch of FIG. 10;

FIG. 10 is an isometric of a straight through mechanical switch in theopen position;

FIG. 10A is an isometric of a straight through mechanical switch in theclosed position;

FIG. 11 is an exploded view of the phased array active antenna system,narrow band electronic countermeasures embodiment;

FIG. 11A is an enlargement of a portion of FIG. 11, phased array activeantenna system, narrow band electronic countermeasures embodiment;

FIG. 12 is an exploded view of the phased array active antenna system,broad band radar embodiment;

FIG. 12A is an enlargement of a portion of FIG. 12, phased array activeantenna system, broad and radar embodiment;

DESCRIPTION OF THE PREFERRED EMBODIMENTS

FIG. 1, is a flowchart of the individual means required for an improvedphased-array active antenna system utilizing a transmit-receive meanscomprising; arrayed transmit-receive cells on a single substrate ofsemiconductor material.

This improved phased array active antenna system 1, comprises a centralprocessing means 2. As shown in FIG. 1, this central processing means 2is operable to generate an RF input signal 3, into the transmit-receivemeans 6. The central processing means 2, also generates coded signals 4to a logic control means 5. The logic control means 5, decodes signal 4into specific voltages. The voltage inputs 6, are then directed to thetransmit-receive means 7. These input voltages 6 from the logic controlmeans 5 will control various phase shifting electronic devices on thetransmit-receive means 7. A direct current power generation means 8located in the system 1, but not on the transmit-receive means 7,generates electrical energy to supply various power amplificationdevices of the transmit-receive means 7. If the phased array activeantenna system 1 is operated in a pulsed mode, a capacitative storagemeans 9, would be located within the system 1, but close to thetransmit-receive means 7. The direct current power generation means 8,used in conjunction with the capacitative storage means 9 would providea direct current energy signal 10 to the transmit-receive means 7 duringactive antenna system 1 operation. This pulsed, direct current energysignal 10 would supply electrical energy to various devices on thetransmit-receive means 7. Heat would be generated by the variousamplification devices on the transmit-receive means 7 during thetransmission of a frequency signal 3. A heat dissipation means 11 woulddissipate the heat away from the transmit-receive means 7. Thetransmit-receive means 7 during a radio frequency signal transmissionwould emit transmission signal 12. Transmission signal 12 would have aspecific, predetermined phase shift and frequency. Transmission signal12 would enter some signal isolation means 13 prior to entering theantenna means 14. Signal isolation means 13 would be operable totransmit or receive a radio frequency in one direction only, i.e., anoutput signal 12 would not be transmitted while a signal 12a was beingreceived by the antenna means 14. The antenna means 14 would be operableto transmit a signal 12, or receive a signal 12a in a predeterminedfrequency range. The received signal 12a would enter thetransmit-receive means 7, where after; amplification, attenuation andphase shifting signal 12a would be transmitted within the system 1 tothe central processing means 2 for analysis.

FIG. 2 is a flowchart of the various means necessary for atransmit-receive means 7 as used in a phased array active antennasystem 1. The central processing means 2 supplies a radio frequencysignal 3 to the transmit-receive means 7. The central processing means 2also supplies a coded logic control signal 4 to the logic control means5. The logic control means decodes the signal 4 and produces inputvoltages 6 to the transmit-receive means 7. The logic control inputvoltage 6, and the radio frequency signal 3 from the central processingmeans 2, enter the transmit-receive means 7 through the attenuator means15, and the various phase shifting devices (digital 20 and analog 25),respectively. The logic control voltages 6 set the phase shiftingdevices 20, 25 to a predetermined phase shift. The attenuator 15receives the radio frequency signal 3 and reduces it. This reducedsignal enters the digital phase shifter 20 where it can be phase shiftedfrom its original phase either zero degrees or a full one hundred andeighty degrees. A digital phase shifter 20 used in conjunction with ananalog phase shifting device 25 would produce a phase shift of a fullthree hundred and sixty degrees. An analog phase shifter 25 is capableof producing a radio frequency phase shift of between zero degreesthrough one hundred and eighty degrees. Transmit-receive switch 30 wouldbe operable as a signal isolation means. The attenuated, phase shiftedsignal 3 would next pass through the transmit-receive switch 30. Whenthis electrically actuated transmit-receive switch 30 is closed, theradio frequency signal 3 would enter into a multi-stage amplifier 35,50, 60. This multi-stage amplifier 35, 50, 60 would boost the amplifieroutput signal 12 to a predetermined power level. A secondtransmit-receive switch 30a would finally receive this amplified signal12 and if switch 30a was in the closed position it would direct theoutput signal 12 to the antenna means 14 for transmission to theenvironment outside the antenna system 1. A signal 12a received by theantenna means 14 would enter the second transmit-receive switch 30a.This signal isolation means 30a would serve to separate the outputsignal 12 and the received signal 12a. An open transmit-receive switch30a would direct the received signal 12a into the low noise amplifierstage 60. This weak, received signal 12a would be amplified in this lownoise amplification stage 60. The amplified signal 12a would then enterthe first transmit-receive switch 30 where if open it would transmitsignal 12a into the analog 25 and digital 20 phase shifting devices.After appropriate phase shifting the radio frequency signal 12a wouldenter into attenuation means 15. After the received signal 12a wasattenuated it would exit the transmit-receive means 7 and enter into thecentral processing means 2 for analysis by the central processing means.

FIG. 3 is a plan view of sixteen individual transmit-receive cells 7 ona single wafer 16 of semiconductor material. The wafer 16 in FIG. 3 isL₁ or approximately 3 inches (7.62 cm) in diameter.

FIG. 3A is a plan view of sixteen individual transmit-receive cells 7 ona single wafer 17 of semiconductor material. The wafer 17 in FIG. 3A isL₂ or approximately 4 inches (10.16 cm) in diameter and isrepresentative of the size of the transmit-receive means 7 array of thepreferred embodiment.

FIG. 3B is an exploded view of an array of sixteen transmit-receivecells 7 all upon an uncut common wafer of semiconductor material. Thedimension L₄ represents a spacing of approximately 0.1 inch (0.254 cm)between each individual transmit-receive cell. Dimension L₅ representsthe approximate width of each transmit-receive cell 7 of 0.395 inches(1.00 cm). The overall length of the common wafer of semiconductormaterial 17, having a four-by-four array of transmit-receive cells wouldbe approximately 2.08 inches (5.28 ). The multi-layer ceramic supportmeans 19 upon which the single layer 17 of semiconductor material ismounted upon is shown in FIG. 3B. In the fabrication of thetransmit-receive cell 7 array, a sealed lid 18 would enclose the surfaceof the transmit-receive cell 7 array.

FIG. 4 is a chart showing the relative positions of the individual,redundant electronic devices on the single transmit-receive cell 7.Specifically, upon this single cell 7 we have an attenuator 15, adigital phase shifter 20, analog phase shifters 25 and 25a, a firsttransmit-receive switch 30, a three stage amplification system 35, 40,50, a low noise amplification system 60 for weak received radiofrequency signals and a second transmit-receive switch 30a. Each stage,35, 40 and 50, of the three stage amplification system is a tripleredundant system. The first stage 35, comprises three distinct firststage amplifiers 35a, 35b, and 35c. The second stage or driver stage 40,comprises amplifiers 40a, 40b and 40c. Finally, the output stageamplifier system 50 comprises three output amplifiers 50a, 50b, 50c.Amplification systems 35, 40 and 50 would be used in the signal transmitcircuit. Low noise amplifiers 60a, 60b, 60c, 60d, 60e, and 60f would beutilized for weak received radio frequency signals. Note: that only oneamplifier in the first stage system 35 need be operational, only oneamplifier of either the driver stage 40 or the output stage 50 and onlytwo of the six low noise amplifiers 60a-60f must function to achieve afully operative transmit-receive cell. Also only one of the two analogphase shifters 25, 25a must function for the transmit-receive cell 7 tooperate.

FIG. 5 is a schematic representation of the individual, redundantelectronic devices on a single transmit-receive cell 7. A signal 3 fromthe radio frequency manifold enters the transmit-receive cell 7 at via21. This signal 3 enters the attenuator 15. The signal 3 is split andenters two legs formed by variable voltage resistors 22, or field effecttransistors. Signal 3 is divided in one half and reflected through thefield effect transistors 22. The reflected summed signal from the fieldeffect transistors 22 is the result of the voltages applied to the fieldeffect transistors 22. The reduced, reflected signal 3 then enters thedigital phase shifter 20. The digital phase shifter which comprises a πnetwork 23 and a coupled line segment 24 utilizes field effecttransistors 26 to switch between the π network 23 and the coupled linesegment 24. If the signal 3 passes through the π network the signal 3will be phase shifted 180° from its input phase. If the signal 3 passesthrough the coupled line segment 24, the signal 3 will be phase shifted0°. The signal 3 enters the analog phase shifter 25 or 25a through amitered mechanical switch 27. This mitered mechanical switch 27 is usedthroughout the transmit-receive cell 7 to selectively interconnectvarious electronic devices. The analog phase shifters 25 or 25a areoperable, utilizing continuously variable varactors having varactordiodes, to phase shift the signal 3 from the digital phase shifter 20from 0° through 180°. The combination of the digital phase shifter 20and one of the analog phase shifters 25 or 25a results in a potential RFsignal phase shift of 0° through 360°. The phase shifted signal 3 nowenters an electrically actuated transmit-receive switch 30. If thistransmit-receive cell 7 is in the transmit mode this switch will beclosed and connected to the transmit circuit and the signal 3 will entera first stage gain control means 31. A gain control means such as alossy equilizer or a lumped element resonator would be used to maintainthe RF signal's 12 gain to a 50Ω system within each amplification stage35, 40 and 50. The first stage gain control means 31 precedes firstamplification stage 35. Three first stage amplifiers 35a, 35b and 36care available for use. The first stage amplifiers 35a, 35b and 35c areall identical having input and output matching circuitry and a 600μfield effect transistor. These amplifiers are capable of producingone-quarter watt of power. Amplified signal 3 enters the driver stagegain control means 39, precedent to entering the driver stage amplifiersystem 40. This stage 40 comprises three independent, redundantamplifiers, 40a, 40b and 40c. Only one amplifier is required at thisstage -- each amplifier has input and output matching circuitry and anequivalent 1200μ field effect transistor. The driver stage amplifiersare capable of producing one-half watt of power. Finally, twiceamplified signal 12 enters output stage amplification system 50 with itsthree amplifiers 50a, 50b and 50c. Again, only one amplifier 50a, 50b or50c need be operational. Each amplifier 50a, 50b or 50c has input andoutput matching circuitry and an equivalent 2400μ field effecttransistor. Each output amplifier 50a, 50b or 50c is operable to produceone full watt of power. The signal 3 now exits the output stage 50 intoa second transmit-receive switch 30a where if this switch is closed,signal 12 will exit the transmit-receive cell through antenna via 33 astransmitted signal 12. A received RF signal 12a enters thetransmit-receive cell through the antenna via 33. This weak signal 12aencounters the second transmit-receive switch 30a. If thetransmit-receive cell 7 is in the receive mode the electrically actuatedtransmit-receive cell 30a will be closed and will direct received signal12a to the low noise amplification stage 60. Only two of the six lownoise amplifiers 60a, 60b, 60c, 60d, 60e and 60f need be operational toboost the weak, received, RF signal 12a. The individual, identical lownoise amplifiers 60a, 60b, 60c, 60d, 60e and 60f comprise; a feed backloop, input and output matching circuitry and a 600μ field effecttransistor. After signal 12a is amplified it enters the firsttransmit-receive switch 30 where if the switch 30 is closed into thereceive circuit signal 12a is directed into the analog phase shifter 25or 25a, the digital phase shifter 20 and finally the attenuator 15.After the attenuator 15, the signal 12a enters the manifold via 21 fortransmittal away from the transmit-receive cell 7 and to the centralprocessing unit 2 for analysis.

FIG. 6 is a chart showing the relative positions of the various groupsof devices as they actually, physically appear on the surface of theindividual transmit-receive cell means. Subsequent FIGS. 6A, 6B, 6C, 6Dand 6E detail the entire surface topography of the cell means.

FIG. 6A is a plan view of the upper left-hand corner of thetransmit-receive cell 7. This FIG. 6A comprises driver stage amplifiers40a and 40b, output amplifier 50a and low noise amplifiers 60a and 60b.Mitered mechanical switches 27 can be seen interconnecting theindividual devices.

FIG. 6B is a plan view of the upper middle quadrant of transmit-receivecell 7. Driver stage amplifier 40c, output power amplifier 50b and lownoise amplifiers 60c and 60d comprise this quadrant and output amplifiergain control means 90. Again, mechanical mitered switches 27interconnect the various devices.

FIG. 6C is a plan view of the upper right-hand corner of thetransmit-receive cell 7. Output amplifier 50c, low noise amplifiers 60eand 60f and the second transmit-receive switch 30a comprise the devicesin this quadrant. The antenna via 33 is shown as a part of the secondtransmit-receive switch 30a.

FIG. 6D is a plan view of the lower left-hand corner and lower middlequadrant of the transmit-receive cell 7. First stage amplifiers 35a, 35band 35c, transmit-receive switch 30, analog phase shifter 25 and firststage gain control means 31, and driver stage gain control means 39comprise the devices in this quadrant.

FIG. 6E is a plan view of the lower right-hand corner of thetransmit-receive cell 7. Analog phase shifter 25a, digital phase shifter20, attenuator 15 and manifold via 21 comprise the devices in thisquadrant.

FIG. 7 is a plan view of the attenuator 15. Eight field effecttransistors 22, are utilized in two groupings of four each. Only onefield effect transistor 22 of each group of four must be operable forthe attenuator to perform during fabrication and test of thetransmit-receive cell 7. Functioning field effect transistors operablein the specified range would be selected and interconnected into theattenuator 15 by straight-through mechanical switches 29. TheWestinghouse patent, U.S. Pat. No. 3,681,134 to Nathanson et al.,teaches a low capacitance configurable switch operable to serve as astraight-through mechanical switch.

FIG. 7A is a plan view of the digital phase shifter 20. The π network 23of the digital phase shifter 20 is operable to phase shift the radiofrequency signal 180° from its received phase. The coupled line segment24 will pass the signal through the digital phase shifter 20 with a 0°phase shift. The field effect transistors 26, 26a occur in two groups ofsix each. Only one field effect transistor of group 26, 26a must beoperable to serve as a field effect transistor switch between the πnetwork 23 and the coupled line segment 24. Straight-through switches 29allow the incorporation of the individual functional field effecttransistors 26 or 26a during transmit-receive cell 7 fabrication andtest. Line 34 is a microstrip direct current distribution line, operableto supply electrical energy to the field effect transistors of 26, 26a.

FIG. 7B is a plan view enlargement of the left side of the digital phaseshifter 20. One-half of the π network 23 is shown as well as one-half ofthe coupled line segment 24. Six field effect transistors 26 offermultiple redundancy and a higher probability of a fully functionaldigital phase shifter 20, because only one must be operational among thesix. Straight-through mechanical switches selectively incorporate eachfunctional, field effect transistor 26. Microstrip line 34 is a directcurrent electrical energy distribution line supply power to the drain orsources of the selected field effect transistors 26.

FIG. 7C is a plan view enlargement of the right side of the digitalphase shifter 20 direct current energy microstrip line 34 supplieselectrical energy to the selected field effect transistor 26A. Only onefield effect transistor 26A of the six need be operational for a fullyfunctional digital phase shifter 20. One half of the π network 23 andone-half of the coupled line segment 24 is seen in this enlargement ofthe right side of the digital phase shifter 20. Straight-throughmechanical switches 29 serve to interconnect the selected field effecttransistor of the group 26A.

FIG. 7D is a plan view of the analog phase shifter 25, 25A. Duringtransmit-receive cell 7 fabrication and test, mitered mechanicalswitches 27 allow a selection of either phase shifter 25 or 25A. Bothphase shifters are identical and both 25 or 25A comprise a coupled linesegment 36, spiral inductances 34, dual field effect transistors 26B anddual capacitors 37. Individual elements are interconnected to form theanalog phase shifter 25 or 25A using straight-through switches 29. Aradio frequency signal 3 received from the digital phase shifter 20 willbe phase shifted either 0°, through the coupled line segment 36 orthrough 180° when passed through the varactor network of spiralinductances 34 and field effect transistors 26B.

FIG. 7E is a plan view of the transmit-receive switch 30, 30a. Thiselectrically actuated switch 30, 30a comprises two legs each of thethree field effect transistors 26c in parallel with spiral inductances34a. Only one field effect transistor 26c of each group of three must befunctional for an operational transmit-receive switch be functional foran operational transmit-receive switch 30, 30a. Again, straight-throughswitches 29 interconnect the selected field effect transistor 26c.

FIG. 7F is a plan view of a first stage amplifier 35a, 35b or 35c. Onlyone of these three amplifiers 35a, 35b or 35c must be operational duringtransmit-receive cell 7 fabrication and test. Each amplifier isidentical to the other two, and comprise, microstrip inductances 41,interconnected to selected capacitors 37, tuning capacitors 37A andradio frequency bypass capacitors 37B. These elements are interconnectedusing straight-through mechanical switches and are operable as input andoutput matching circuitry. The "heart" of the first stage amplifier,35a, 35b or 35c is a 600μ field effect transistor 38. This 600μ fieldeffect transistor 38 is operable to produce an output signal ofone-quarter watt of power.

FIG. 7G is a plan view of the driver stage amplifier 40, 40b and 40c.Only one of these three amplifiers 40a, 40b and 40c must be operationalduring transmit-receive cell 7 fabrication and test. Each amplifier isidentical to the other two, and comprise, microstrip inductances 41,interconnected to selected capacitors 37, and tuning capacitors 37A toform input and output matching circuitry. The "heart" of the driverstage amplifier are two field effect transistors 38. Each field effecttransistor has a value of 600μ and are connected utilizing Westinghousepatented "cluster matching" technique, U.S. Pat. No. 4,547,745, toFreitag et al., this combination of two field effect transistors 38results in a combined value of 1200μ with a resultant output power levelof one-half watt of power. Therefore the output radio frequency signal12 issued from the selected driver stage amplifier will have an outputpower of one-half watt. Again, straight-through switches 29 interconnectthe matching circuitry elements, as necessary. The term "μ" whenreferring to a field effect transistor 38 refers to the width of thechannel of the field effect transistor 38 and its resultant power outputcapabilities.

FIG. 7H is a plan view of the output stage amplifier 50a, 50b and 50c.Again, only one of the output stage amplifiers 50a, 50b or 50c need beoperational for the amplification of the radio frequency signal 3 to onefull watt of power. Input and output matching circuitry comprisingvarious capacitors 37, tuning capacitors 37a, and microstrip inductancelines 41 are interconnected as necessary by straight-through switches29. Four field effect transistors 38, each having 600μ field effecttransistors results in a total value of 2400μ. The output amplifier 50a,50b, or 50c is equal to two one-half watt amplifiers in parallel. Theradio frequency signal 12 will achieve one full watt of power from thisoutput stage amplifier 50a, 50b and 50c.

FIG. 7I is a plan view of the low noise amplifiers 60a, 60b, 60c, 60d,60e and 60f. The six low noise amplifiers 60a, 60b, 60c, 60d, 60e and60f are operable to receive the weak radio frequency signal 12a from theenvironment outside of the active antenna system 1. Only two of the sixlow noise amplifiers are required to be operational for amplification ofreceived signal 12a. The low noise amplifiers 60a, 60b, 60c, 60d and 60f60f comprise input and output matching circuitry such as microstripinductances 41, capacitors 37, tuning capacitors 37a and straight lineswitches 29. A blocking capacitor 37c functions as an integral part of afeedback loop 42. The received signal 12A will feedback into the 600μfield effect transistor 38a. This field effect transistor 38a isdistinct from the previously described field effect transistors 38. Theprevious field effect transistors 38, had gate lengths of approximately0.8μ. This gate length of 0.8μ is most applicable to field effecttransistors in the power amplification mode. Field effect transistor 38aof the low noise amplifiers 50a, 60b, 60c, 60d, 60e and 60f have gatelengths of approximately 0.5μ. This gate length of 0.5μ provides lessnoise and higher gain for the received amplified signal 12a. In summary,the low noise amplifiers 60a, 60b, 60c, 60d, 60e and 60f are standardfeedback amplifiers utilizing field effect transistors 38a, providingone-quarter watt of output power with increased signal gain and reducednoise.

FIG. 8 is a cross section of the manner of making the vias 21, 33 whichbring signals from the bottom surface of the semiconductor wafer 17 tothe top surface of that same semiconductor wafer 17. Via 21 is themanifold via which brings a radio frequency signal up through thesemiconductor wafer 17 and across the microstrip upon the surface of thetransmit-receive cell 7 into the attenuator 15. The antenna via 33 takesthe radio frequency output signal 12 of approximately one watt from thesecond transmit-receive switch through the semiconductor wafer 17 and tothe antenna means 14 for transmission outside of the active antennasystem 1. A recommended fabrication method for these vias 21, 33 wouldproduce solid electrical connections that could be repaired ifimproperly formed during transmit-receive cell fabrication. One methodof via fabrication would utilize a metal evaporation technique. FIG. 8shows a wafer of semiconductor material 17, i.e., gallium arsenide. Thesingle wafer 17 would be thinned down to a thickness of approximately100μ, as used in microwave circuitry. Wafer 17 would be mounted facedown on wafer holder 45 using a soft wax 46 as an adhesive. Photoresistlayer 47 is then applied to the waver 17. The photoresist 47 is thenpatterned to define the holes through which the vias 21, 33 would beetched. Vias 21, 33 formed through a gallium arsenide wafer 17 could beformed using wet chemical etching or reactive ion etching. Shown incross section in FIG. 8 is a single field effect transistor 38, having asource 43 and drain 44.

Next, the photoresist mask 47 is removed and metal is sputtered over thebottom surface of wafer 17 forming a metalization layer 48 as shown inFIG. 8A, a cross section of the manner of making the via connections 21,33. A second layer of photoresist 4a is patterned about via 21, 33.

FIG. 8B is a cross section manner of making demonstrating the removal ofthe second layer of photoresist 47a after a layer 51 of Au, or othersimilar highly conductive metal. When the second photoresist layer 47ais removed the thin-sputtered metal layer 48 is exposed. The removal ofthe second photoresist layer 47a can be performed by etching orion-milling. The gallium arsenide wafer 17 is then lightly etched toclean the surface and insure its insulating properties. Gaps formed bythe removed second layer of photoresist 47a are gaps 52, 52a and 52b.

FIG. 8C is a cross section method of making wherein the wafer 17 isdemounted from wafer holder 45 and wax 46 is removed. The heat sink 53for wafer 17 comprises a previously prepared wafer of aluminum nitride53. This heat sink 53 should be of a semi-insulating material, havinggood thermal conductive properties and an expansion coefficient closelymatched to the wafer 17, in this case, gallium arsenide. Close matchingbetween wafer 17 and heat sink 53 will prevent cracking of the wafer 17during thermal cycling. Solder 54 will serve to attach the aluminumnitride heat sink 53 to the gallium arsenide wafer 17.

FIG. 8D is a cross section manner of making wherein a metal shadow mask55 is used to define the metal 57 evaporated through the orifice 56 inthe mask 55. The first layer 58 and second layer 59 of the mask 55 areselectively etched to form orifice 56 which by its size defines themetal evaporation layer 57. Holes 52 and 52a are partially filled byevaporated metal 57. Gap 52b is not filled with evaporated metal 57 andremains open. Additional metal 57 may be evaporated into the areadefined by orifice 56 is there is insufficient metalization duringinitial fabrication to make a good contact.

FIG. 8E is a cross section manner of making of the aluminum nitridelayers 53, 53a and 53b. Heat sink layer 53 serves as a structuralsupport and heat dissipation means for the gallium arsenide wafer 17.Layer 53a comprises a second layer of aluminum nitride and a laserdrilled, metalized "T" contact 61. The planar top surface of "T" contact61 contacts contact points 57a and 57b of metal evaporation contact 57.A third layer of aluminum nitride 53b comprises a Duroid, layer 62 ofmanifold material. During via 21, 33 operation a signal either radiofrequency or direct current will enter the surface layer of thetransmit-receive cell 7 devices through the metalization contact 57,from manifold 62, through "T" contact 61. This technique while not theexclusive method to manufacture vias 21, 33 will produce a high yield ofsuccessful contacts and facilitate re-metal evaporation of area 57 toincrease or build up the contact.

FIG. 9 is a plan view of the mitered mechanical switch 27 whichfacilitates the interconnection of selected electronic devices on thesurface of the transmit-receive cell 7. Mitered mechanical switch 27comprises three layers of distinct metalization, layers 27a, 27b and27c.

FIG. 9A is a plan view of first metalization layer 27a. Firstmetalization layer 27a comprises three distinct portions; 27a1, arectangular piece with a beveled left lower corner; 27a2 the left halfportion of a bisected rectangle; and 27a3, the right half portion of abisected rectangle.

FIG. 9B is a plan view of the second metalization layer 27b. Secondmetalization layer 27b comprises three distinct portions; 27b1, arectangular piece substantially smaller than 27a1; 27b2 the left halfportion of a bisected rectangle, also slightly smaller in size than27a2; and 27b3 the right half portion of a bisected rectangle, againsmaller in physical size than 27a3. During fabrication of thetransmit-receive cell 7, metalization layer 27b will be layered uponlayer 27a.

FIG. 9C is a plan view of the third metalization layer 27c. Thirdmetalization layer 27c comprises three distinct portions; 27c1 arectangular piece significantly smaller than 27b1; 27c2 the left halfportion of a bisected rectangle, significantly smaller than 27b2; and akeystone shaped portion 27c3. This 27c3 keystone portion issignificantly larger than 27b3. During fabrication of the miteredswitches 27 on the transmit-receive cell 7, metalization layer 27c willbe layered upon layer 27b.

FIG. 9D is a left side view of mitered switch 27 as shown in FIG. 9. Anair gap or air path 28 can be seen formed between layers 27c3 and 27a1.When this air path or gap 28 exists the switch is open and no electricalor radio frequency energy will pass through mitered switch 27.

FIG. 9E is a right side view of mitered switch 27 as shown in FIG. 9. Anair path or air gap 28 is found between metalization layers 27c3 and27a. If this switch 27 is open this air path 28 will be open.

FIG. 9, in summary, is a plan view of mechanical mitered switch 27.During transmit-receive cell 7 fabrication and test various redundantelectronic devices will be found operative or inoperative. Selectedelectronic devices may be permanently interconnected together formingtransmit or receive circuits using the mechanical mitered switch 27. Aswitch 27 would be placed at the input and the output of each device. Toclose switch 27, to interconnect a specific device, portion 27c3 ofmetalization layer 27c must be actuated using pressure or vibration.Once layer 27c3 contacts layer 27a1 the switch will be closed forming aright angle switch. If a particular device is to be bypassed in thecircuit, portion 27c3 must contact layer 27a2 -- only the lower "head"of the keystone 27c3 is contacted to 27a2 creating a straight-throughelectrical line connection between 27c3 and 27a2.

FIG. 10 is an isometric view of a low capacitance configurable or"straight-through" switch. Such a switch interconnects the various fieldeffect transistors or capacitors within the individual electronicdevices. This switch, which comprises two portions, 29a and 29b, isoperable to be cold vibration welded into a closed position. FIG. 10shows the low capacitance configurable switch in the open position.Portion 19a could be some type of gold alloy like AuTi. Portion 29awould have a width of L₆ or approximately, 0.005 inches (0.013 cm).Portion 29b would be layered of Au only, and having a width L₇ ofapproximately 1.5μ. The gap between portion 29a and portion 29b when theswitch 29 is in the open position would be approximately 5μ or dimensionL₈. When in the open position, switch 29 will have portion 29aoverhanding portion 29b by approximately 0.0025 inches (0.006 cm).

FIG. 10a is an isometric view of the low capacitance switch 29 in theclosed position. When switch 29 is subjected to vibration at roomtemperature and permanent cold weld is formed between portion 29a and29b. A portion of 29b of length L₉ or approximately 0.0025 inches (0.006cm). This low capacitance configurable switch is taught by the U.S.Patent to Nathanson et al., assignee Westinghouse Electric Corporation,U.S. Pat. No. 3,671,134.

FIG. 11 is an exploded view of an active, phased array antenna systemhaving electronic countermeasure applications, 1a. Logic control devices5 rest upon the underside of sealed lid 18. Sealed lid 18 is operable tofully enclose the array of transmit-receive cells 7 all formed, uncutupon the single wafer of gallium arsenide 17. The logic control devices5 feed their decoded voltages from the central processing unit 2 throughlines 63 to strap 64. Strap 64 interconnects the voltages from the logiccontrol devices 5 to the lines 65 between the individualtransmit-receive cells 7. The wafer 17 comprising the array oftransmit-receive cells 7 rests upon a multilayer aluminum nitridesupport layer 17. The multilayer support layer 19 comprises aluminumheat sink 53 and sublayers 53a and 53b. Input and output vias 21, 33 forthe radio frequency signal or direct current energy are cut into thecommon wafer 17 for each individual transmit-receive cell 7. Electricalinterconnection between the surface of wafer 17 and the underlying RFmanifold 67 and direct current manifold 66 is achieved through the useof multistage metal evaporated vias 57, 61 and 62. Radio frequencysignals 12 transmitted from this electronic countermeasuretransmit-receive cell 7 would exit the RF manifold 67 by hardwire 68which is connected to one horn of broadband antenna means 14a. A receiveradio frequency signal, 12A would enter horn 14a and pass into theantenna via by hardwire 69. A broadband application would be in therange of 2 GHz to 20 GHz. A signal 12A in this range would be receivedby the horn antenna means 14a. Receipt of such a signal 12a wouldindicate that an enemy radar system was in the environment outside ofthe active antenna system 1A. The received signal 12A would pass upthrough the various support structures of system 1A into the RF manifold67, up through via 57 by way of contacts 61 and 62. The input signal 12Awould enter the surface of the transmit-receive cell 7 where the receivecircuit would low noise amplify, attenuate, phase shift, analog ordigitally dependent upon the logic control means 5 as directed by thecentral processing means 2. The received signal 12a would then pass intothe manifold 11 and into the central processing means 2. During thetransmission mode of an amplified radio frequency signal 12, heat isproduced by the output stage amplifiers on the transmit-receive cell 7.This heat is effectively dissipated by the heat dissipation means 11.The active antenna ECM (electronic counter measures) system 1A canoperate in the pulsed mode by the storage of electrical energy in thecapacitative storage means 9. A transmitted signal 12 in this systemwill be transmitted, cross polarized from the enemy signal 12a therebyeffectively jamming his radio frequency transmissions 12a.

FIG. 11A is a cross section enlargement of the ECM active antenna system1A. Sealed lid 18 has logic control means 5 embedded upon it. Trap 64carries the decoded voltages from the logic control means to thetransmit-receive cell 7 which rests upon AlN layer 19. Upon theunderside of AlN layer 19, a capacitative storage means 9 storeselectrical energy for pulsed operation. Electrical connection 7transmits this stored energy from storage means 9 to the individualtransmit-receive cell 7. Heat dissipation means 11 with a multiplicityof orifices 71 dissipates heat buildup away from the transmit-receivecell 7. The antenna means 14a comprises dual horns which are operable totransmit signals polarized from the signals received. Received signalstravel from one horn of antenna 14a in line 68. Transmitted signals passthrough line 69 to the second horn of antenna 14A.

FIG. 12 is an exploded view of a radar application for the activeantenna phased array system 1B. This narrow band application wouldbroadcast in a range of approximately 9.8 GHz to 10.2 GHz. A patchantenna means 14B would transmit 12 or receive the reflected signal 12a.A sealed cover means 18 having a multiplicity of logic control means 5embedded in its surface would fully enclose the gallium arsenide wafer17 with its multiplicity of individual transmit-receive cells 7. Eachtransmit-receive cell is operable to, utilizing one logic control means5 and one antenna means 14b transmit or receive a radio frequency signalof predetermined phase and frequency. Logic control signals, in the formof voltages are sent by common lines 63 through strap 64 to wafersurface lines 65. These logic control voltages direct the individualphase shifting devices on the transmit-receive cell 7. Eachtransmit-receive cell 7 has a multiplicity of electronic devices uponits surface, which are fully redundant and operable to be selectively,permanently interconnected to form distinct transmit or receivecircuits. The wafer 17 is supported by a multilayer AlN supportstructure 19. This structure 19 further comprises 53, 53a and 53b. Vias21, 33 formed of elements 57, 61 and 62 interconnect the surface of thewafer 17 and the embedded radio frequency 67 and direct currentmanifolds 66. Direct current energy is stored in capacitative storagemeans 9, and supplied to the cells 57 during pulsed signal transmission.Heat generated by the output amplifiers on the transmit-receive cell 7,is dissipated by heat dissipation means 11 through orifices 71. Atransmitted signal 12 will pass from the RF manifold 67 by line 72 toantenna means 14b. The received, weak reflected signal 12a will pass onthe same line 72 to the same RF manifold 67. Received signal 12a will bepassed to the surface of the transmit-receive cell 7 by way of vias 21,33 and to the central processor 2 for analysis.

FIG. 12A is a cross section enlargement of the radar, narrow band,active antenna system 1a. Sealed lid 18 has logic control means 5embedded upon it. Strap 64 carries the decoded voltages from the logiccontrol means to the transmit-receive cell 7 which rests upon AlN layer19. Upon the underside of AlN layer 19, a capacitative storage means 9stores electrical energy for pulsed operation. Electrical connection 70transmits this stored energy from storage means 9 to the individualtransmit-receive cell 7. Heat dissipation means 11 with a multiplicityof orifices 71 dissipates heat buildup away from the transmit-receivecell 7. The antenna means 14B comprises a patch antenna or flat circulardisk, off center actuated which is operable to transmit signals orreceive signals in the narrow band range. Received signals travel fromthe patch antenna 14B in line 72 to the cell 7. Transmitted signals passthrough line 72 to the same patch antenna 14B and into the environmentoutside of the system 1B.

Numerous variations may be made in the above-described combination anddifferent embodiments of this invention may be made without departingfrom the spirit thereof. Therefore, it is intended that all mattercontained in the foregoing description and the accompanying drawingsshall be interpreted as illustrative and not in the limiting sense.

We claim:
 1. Miltered mechanical switches comprising:a firstmetallization layer having at least three distinct means: a first layerfirst means configured as a rectangle having one beveled corner, a firstlayer second means on the same plane as said first layer first means,located directly across from said bevel of said first layer first means,said first layer second means configured as a bisected rectangle, and afirst layer third means, said first layer third means also configured asa bisected rectangle, said first layer third means resting upon the sameplane as said first layer first and second means, further said bisectedfirst layer third means positioned directly opposed from said firstlayer first means and beside said first layer second means, a secondmetallization layer, said second metallization layer having at leastthree distinct means: a second layer first means, said second layerfirst means being configured as a rectangle, further said second layerfirst means being smaller in size than said first layer first means, andsaid second layer first means operable to be layered upon said firstlayer first means such that a portion of said first layer first means isnot covered by said second layer first means, a second layer secondmeans, said second layer second means being configured as a bisectedrectangle, further said second layer second means being smaller in sizethan said first layer second means, and said second layer second meansoperable to be layered upon said first layer second means such that aportion of said first layer second means is not covered by said secondlayer second means, and a second layer third means, said second layerthird means being configured as a bisected rectangle, further saidsecond layer third means being smaller in size than said first layerthird means, and said second layer third means operable to be layeredupon said first layer third means such that a portion of said firstlayer third means is not covered by said second layer third means, and athird metallization layer, said third metallization layer having atleast three distinct means: a third layer first means, said third layerfirst means being configured as a rectangle, further said third layerfirst means being smaller in size than said second layer first means,and said third layer first means operable to be layered upon said secondlayer first means such that a portion of said second layer first meansis not covered by said third layer first means, a third layer secondmeans, said third layer second means being configured as a bisectedrectangle, further said third layer second means being smaller in sizethan said second layer second means, and said third layer second meansoperable to be layered upon said second layer second means such that aportion of said second layer second means is not covered by said thirdlayer second means, and a third layer third means said third layer thirdmeans configured like two, off-centered interconnected, bisectedrectangles, forming a head portion and a tail portion, said head portionof said third layer third means operable to be layered upon said secondlayer third means such that portion of said head portion of said thirdlayer third means is parallel to, but not resting upon said first layersecond means and said first layer third means, and said tail portion ofsaid third layer third means is operable to be parallel to but notresting upon said first layer first means, further said third layerthird means operable to be physically deflected in a downward manner atsaid head and aid tail portions such that the deflection of said headportion would cause said head portion to be permanently interconnectedto said first layer second means and said first layer third means andfurther said tail portion deflection would permanently interconnectedsaid tail portion to said first layer first means.